Patents by Inventor Benoit Fleury

Benoit Fleury has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 11952438
    Abstract: A 1,3-dipolar compound including an epoxide group is provided. The epoxide group is a 3-membered ether ring in which a first member is a carbon atom having an attachment to the dipole of the 1,3-dipolar compound and a second member is a tertiary or quaternary carbon. The use of the 1,3-dipolar compound in the modification of a diene polymer makes it possible to improve the rupture properties of a rubber composition comprising the modified polymer, without the expense of its hysteresis properties, while at the same time improving its implementation.
    Type: Grant
    Filed: November 20, 2018
    Date of Patent: April 9, 2024
    Assignee: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN
    Inventors: Anne-Frédérique Salit, Benoît Schnell, Sophie Gander, Sergey Ivanov, Etienne Fleury
  • Patent number: 10630093
    Abstract: A method for optimizing the architecture of the power supply of a load, includes the following steps: determination of a mission profile (16) sizing according to the power required by the load over time; definition of the sources of energy storage for hybridization; association of a characteristic behavior model with each source of energy storage; determination of the couples of sources of energy storage that can generate the mission profile with a minimum mass; and determination, from the potential couples of sources of energy storage, of the couple with the weakest mass.
    Type: Grant
    Filed: September 30, 2014
    Date of Patent: April 21, 2020
    Assignees: AIRBUS GROUP SAS, AIRBUS DEFENCE AND SPACE SAS, AIRBUS HELICOPTERS
    Inventors: Benoit Fleury, Gregor Massiot, Pierre-Bertrand Lancelevee, Julien Labbe
  • Patent number: 10050439
    Abstract: A device (10) for the electric power supply of a load (11), includes at least two energy storage elements (13, 14), elements for determining the power needs of the load (11), elements (16, 17) for monitoring each energy storage element (13, 14), which are able to provide information about a maximum instantaneous power of each energy storage element (13, 14), a calculation body (19) for determining a maximum secured power according to the electromotive force (Ebat(t)) and the resistance (Rbat(t)) of the Thévenin model, a maximum specified current and a maximum specified voltage, and elements (Cbat(t), Csc(t)) for controlling each energy storage element (13, 14), the elements being adjusted over time according to the power needs of the load (11) and the maximum secured power of each energy storage element (13, 14).
    Type: Grant
    Filed: September 30, 2014
    Date of Patent: August 14, 2018
    Assignees: AIRBUS GROUP SAS, AIRBUS DEFENCE AND SPACE SAS
    Inventors: Benoit Fleury, Gregor Massiot, Pierre-Bertrand Lancelevee, Julien Labbe
  • Patent number: 9643713
    Abstract: A method of manufacturing a stiffened panel having a skin and at least one substantially elongate stiffener having a longitudinal groove forming a cavity. At least one storage device for storing and releasing electrical energy. The longitudinal groove is filled with at least one storage device for storing and releasing electrical energy. The storage device is covered with a skin which forms the cavity together with the longitudinal groove of the stiffener. A stiffened ring can be derived from the method.
    Type: Grant
    Filed: September 9, 2013
    Date of Patent: May 9, 2017
    Assignee: AIRBUS GROUP SAS
    Inventors: Michel Bermudez, Didier Mesnage, Hichem Smaoui, Benoit Fleury
  • Publication number: 20160248267
    Abstract: A method for optimizing the architecture of the power supply of a load, includes the following steps: determination of a mission profile (16) sizing according to the power required by the load over time; definition of the sources of energy storage for hybridization; association of a characteristic behavior model with each source of energy storage; determination of the couples of sources of energy storage that can generate the mission profile with a minimum mass; and determination, from the potential couples of sources of energy storage, of the couple with the weakest mass.
    Type: Application
    Filed: September 30, 2014
    Publication date: August 25, 2016
    Inventors: Benoit FLEURY, Gregor MASSIOT, Pierre-Bertrand LANCELEVEE, Julien LABBE
  • Publication number: 20160233672
    Abstract: A device (10) for the electric power supply of a load (11), includes at least two energy storage elements (13, 14), elements for determining the power needs of the load (11), elements (16, 17) for monitoring each energy storage element (13, 14), which are able to provide information about a maximum instantaneous power of each energy storage element (13, 14), a calculation body (19) for determining a maximum secured power according to the electromotive force (Ebat(t)) and the resistance (Rbat(t)) of the Thévenin model, a maximum specified current and a maximum specified voltage, and elements (Cbat(t), Csc(t)) for controlling each energy storage element (13, 14), the elements being adjusted over time according to the power needs of the load (11) and the maximum secured power of each energy storage element (13, 14).
    Type: Application
    Filed: September 30, 2014
    Publication date: August 11, 2016
    Applicants: Airbus Group SAS, Airbus Defense and Space SAS
    Inventors: Benoit FLEURY, Gregor MASSIOT, Pierre-Bertrand LANCELEVEE, Julien LABBE
  • Publication number: 20150225073
    Abstract: A method of manufacturing a stiffened panel having a skin and at least one substantially elongate stiffener having a longitudinal groove forming a cavity. At least one storage device for storing and releasing electrical energy. The longitudinal groove is filled with at least one storage device for storing and releasing electrical energy. The storage device is covered with a skin which forms the cavity together with the longitudinal groove of the stiffener. A stiffened ring can be derived from the method.
    Type: Application
    Filed: September 9, 2013
    Publication date: August 13, 2015
    Applicant: AIRBUS GROUP SAS
    Inventors: Michel Bermudez, Didier Mesnage, Hichem Smaoui, Benoit Fleury